Difference between revisions of "Lunar Reconnaissance Orbiter (BrianJ add-on)"

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== Overview ==
 
== Overview ==
The Lunar Reconnaissance Orbiter (LRO) is the first mission in NASA's planned return to the moon. LRO will launch 2nd March, 2009, with the objectives to finding safe landing sites, locate potential resources, characterize the radiation environment and test new technology.
+
The Lunar Reconnaissance Orbiter (LRO) is the first mission in NASA's planned return to the moon. LRO is scheduled to launch 24th April, 2009, with the objectives to finding safe landing sites, locate potential resources, characterize the radiation environment and test new technology.
  
 
The return to the moon will enable the pursuit of scientific activities that address our fundamental questions about the history of Earth, the solar system and the universe -- and about our place in them. It will allow us to test technologies, systems, flight operation and exploration techniques to reduce the risk and increase the productivity of future missions to Mars and beyond. It will also expand Earth's economic sphere to conduct lunar activities with benefits to life on our home planet.
 
The return to the moon will enable the pursuit of scientific activities that address our fundamental questions about the history of Earth, the solar system and the universe -- and about our place in them. It will allow us to test technologies, systems, flight operation and exploration techniques to reduce the risk and increase the productivity of future missions to Mars and beyond. It will also expand Earth's economic sphere to conduct lunar activities with benefits to life on our home planet.
Line 19: Line 19:
 
Earth’s closest neighbor is holding a secret. In 1999, hints of that secret were revealed in the form of concentrated hydrogen signatures detected in permanently shadowed craters at the lunar poles by NASA’s Lunar Prospector. These readings may be an indication of lunar water and could have far-reaching implications as humans expand exploration past low-Earth orbit. The Lunar CRater Observing and Sensing Satellite (LCROSS) mission is seeking a definitive answer.
 
Earth’s closest neighbor is holding a secret. In 1999, hints of that secret were revealed in the form of concentrated hydrogen signatures detected in permanently shadowed craters at the lunar poles by NASA’s Lunar Prospector. These readings may be an indication of lunar water and could have far-reaching implications as humans expand exploration past low-Earth orbit. The Lunar CRater Observing and Sensing Satellite (LCROSS) mission is seeking a definitive answer.
  
=== required add-ons ===
+
=== Required add-ons ===
* [http://orbithangar.com/searchid.php?ID=2601 Atlas V heavy] V2 by Kev33
+
* [http://users.kymp.net/p501474a/Orbiter/Orbiter.html IMFD 4.2.2]
* [http://koti.mbnet.fi/jarmonik/Orbiter.html IMFD 5.1m]
+
* [http://orbithangar.com/showAddon.php?id=f12093c1-4d5e-4a57-b2e2-427a205f82ee Multistage2015 for Orbiter 2010] (install the add-on and copy "Multistage2015.dll" under the "Modules" folder to "Multistage2.dll")
  
=== optional add-ons ===
+
=== Optional add-ons ===
  
 
* [http://orbithangar.com/searchid.php?ID=3165 Attitude MFD]  
 
* [http://orbithangar.com/searchid.php?ID=3165 Attitude MFD]  
* [http://www.orbithangar.com/searchid.php?ID=2989 Telescope MFD]
+
* [http://orbithangar.com/searchid.php?ID=3434 Level 9 Lunar Texture] or [http://www.orbithangar.com/searchid.php?ID=3570 Moon3d by BrianJ]
* [http://orbithangar.com/searchid.php?ID=3434 Level 9 Lunar Texture] or [http://library.avsim.net/download.php?DLID=99407 Moon3d by BrianJ]
+
 
 +
== Spacecraft Specifications ==
 +
 
 +
'''LRO'''
 +
*Empty Mass 809kg
 +
*Fuel Mass 897kg, ISP 2100Ns/kg
 +
*Main Engine 352N
 +
*RCS 20N
 +
 
 +
 
 +
'''LCROSS'''
 +
*Empty Mass 592kg
 +
*Fuel Mass 300kg, ISP 2200Ns/kg
 +
*Retro Engine 44N
 +
*RCS 4.5N
 +
 
 +
 
 +
'''AV020Centaur'''
 +
*Empty Mass 1914kg
 +
*Fuel Mass 20672kg, ISP 4200Ns/kg
 +
*Main Engine 99400N
 +
*RCS 1000N
 +
 
 +
'''NOTE''': When AV020Centaur fuel is finished, control is automatically switched to LCROSS propulsion system.
 +
 
 +
== Spacecraft Controls ==
 +
Available commands are displayed on the top-left of the vessel HUD
 +
 
 +
'''AV020Centaur'''
 +
 
 +
{{Key|P}} = Toggle Parking Orbit Autopilot On/Off<br>
 +
{{Key|J}} = Jettison LRO<br>
 +
{{Key|B}} = Manual Purge Centaur Fuel (automatic at 32000km alt.)<br>
 +
{{Key|K}} = Jettison LCROSS<br>
 +
{{Key|V}} = Deploy/Delete LCROSS "Bullseye" target on Moon N.Pole<br>
 +
{{Key|N}} = Display LRO Lunar Orbit Data<br>
 +
{{Key|M}} = TransX cheat! Enable 44N "ghost" Main Engine for use with TransX
 +
 
 +
 
 +
'''LRO'''
 +
 
 +
{{Key|G}} = Deploy Antenna (automatic Earth tracking)<br>
 +
{{Key|K}} = Deploy Solar Panel (automatic Sun tracking)<br>
 +
{{Key|N}} = Activate Laser Altimeter<br>
 +
{{Key|V}} / {{Key|Shift}}{{Key|V}} = Rotate DLRE Azimuth<br>
 +
{{Key|B}} / {{Key|Shift}}{{Key|B}} = Rotate DLRE Elevation
 +
 
 +
 
 +
'''LCROSS'''
 +
 
 +
{{Key|F8}} = View from Visual Context Imager (6 deg FOV)
 +
 
 +
 
 +
'''LC-41 (Launch Pad)'''
 +
 
 +
{{Key|V}} = LOX Vent On/Off<br>
 +
{{Key|K}} = Lights Off<br>
 +
'''NOTE:''' LC-41 is automatically deleted when focus vessel is above 100km alt.
 +
 
 +
== Add-on Notes and Quick Info ==
 +
'''NOTES'''
 +
 
 +
''Moon Orientation''<br>
 +
The precession of the Moon's axis is not modelled in Orbiter. To ensure accuracy of the Moon's orientation at the time of the mission, the LRO add-on uses a custom sol.cfg and moon.cfg located in the Config/LRO/ directory. To use them, the "Environment" entry in the scenario file must point to the LRO/sol.cfg.
 +
e.g.
 +
BEGIN_ENVIRONMENT
 +
  '''System LRO/Sol'''
 +
  Date MJD 54892.2256944444
 +
END_ENVIRONMENT
 +
 
 +
 
 +
''Launch Date''<br>
 +
Although the launch is currently scheduled for 24th April 2009, the primary launch scenario provided in this add-on is the 27th April 2009 due to the mission constraints on the LAN of LRO's final Lunar orbit. The second launch scenario provided is for the 24th April 2009, should you wish to use it.
 +
 
 +
''Transx version''<br>
 +
This document assumes the default Transx version supplied with Orbiter. Other versions may give different lunar intercept times.
 +
 
 +
 
 +
'''QUICK INFO'''
 +
 
 +
''LRO''<br>
 +
Final Lunar orbit - 30km x 70km, 90deg inclination(Equatorial), Periselene over South Pole,<br>
 +
LAN = 38deg(Ecliptic) +/- 17deg(max.)
 +
 
 +
 
 +
''LCROSS/AV020Centaur''<br>
 +
Uses Lunar flyby to reach high-inclination Earth orbit,<br>
 +
Spacecraft:Moon orbit resonance 2:3 (other resonances possible)
 +
 
 +
Impact chosen target at North Pole of Moon (targets designated by surface bases "Lcross_A" to "Lcross_E"),  impact speed ~2.5km/s, impact angle > 60deg.
 +
 
 +
Lcross separates from AV020Centaur at impact -9hrs. Lcross impact 4mins after AV020Centaur.
 +
 
 +
Impact should be timed to be visible by LRO passing over and by ground-based observers in Hawaii during hours of darkness.
  
 
== Procedures ==
 
== Procedures ==
 
Accuracy of burns in this mission is '''CRITICAL'''.  
 
Accuracy of burns in this mission is '''CRITICAL'''.  
During this mission, especially after the TLI burn, we will be using the tools TransX or IMFD to get the '''DIRECTION''' of our burns, and using IMFD map to monitor in real time the '''MAGNITUDE''' of the DeltaV we are imparting. For this mission, usually the AUTOBURN button is '''NOT''' your friend.
 
  
You may wish to edit your config/Moon.cfg file and change the LAN line to
 
LAN = 2.2483                    ; ascending node of equator - CHECK!
 
This will ensure a more accurate simulation. 
 
 
=== Launch ===
 
=== Launch ===
  
Fire up the '''01 - AV020 LRO launch''' scenario in the LRO scenarios folder
+
Fire up the '''01 - AV020 LRO launch 27Apr''' scenario in the LRO scenarios folder
 
This is a night launch so visibility is poor until after the TLI burn.  
 
This is a night launch so visibility is poor until after the TLI burn.  
The scenario starts at UTC 03/02/2009 05:25:00.
+
The scenario starts at UTC 04/27/2009 04:09:00.
Launch time is UTC 05:26:27.
+
Launch time is UTC 04:10:11.
 
The default camera view is Ground Observer. You have just over a minute to set up the camera to your personal preference.
 
The default camera view is Ground Observer. You have just over a minute to set up the camera to your personal preference.
  
  <nowiki>At UTC 05:26:17 press the</nowiki> '''p''' <nowiki>key to start the launch countdown and 1st stage auto-pilot.</nowiki>
+
  At UTC 04:10:01 press the '''p''' key to start the launch countdown and  
 +
1st stage auto-pilot.
  
 
At T-5 seconds, engine ignition will happen, and the hold down clamps release at T-0.
 
At T-5 seconds, engine ignition will happen, and the hold down clamps release at T-0.
Line 60: Line 150:
  
 
  Also, click the '''HUD''' button in the right ''orbit'' MFD so that your HUD is set to orbit reference Earth
 
  Also, click the '''HUD''' button in the right ''orbit'' MFD so that your HUD is set to orbit reference Earth
 +
Click the '''Prograde''' button to engage the prograde autopilot.
  
 
==== IMFD Configuration set-up ====
 
==== IMFD Configuration set-up ====
Line 74: Line 165:
 
  Click '''Set'''
 
  Click '''Set'''
 
  Click '''Tgt''' and enter '''Moon'''
 
  Click '''Tgt''' and enter '''Moon'''
  Click '''Nxt''' so that the ''Tej'' parameter is highlighbted.
+
  Click '''Nxt''' 6 times so that ''Off Plane'' is highlighted.
  Click + or - repeately until the ''dV'' parameter reaches a minimum. This should be about ''3.13k''
+
Click '''+''' twice to change it to ''Source Plane''.
  Click '''Pg''', then '''BV''', then '''AB'''
+
Click '''Prv''' so that ''Realtime'' is higlighted.
 +
Click '''+''' to change it to ''Off-Axis''
 +
Click '''Prv''' twice so that ''TIn'' is highlighted.
 +
Click '''+''' or '''-''' repeatedly to minimize the value of ''PlC'' in the lower left section of the MFD.
 +
You may want to click on '''ADJ''' and set it to ''10x'' for this adjustment.
 +
Be sure to set it back to ''1x'' when finished.
 +
Click '''Prv''' twice so the ''Tej'' parameter is highlighted.
 +
  Click '''+''' or '''-''' repeatedly until the ''EjA'' parameter is about 3 degrees.
 +
If you go much below 3 degrees the ''Off-Axis'' parameter will change back to ''Realtime'',
 +
and we need to be in ''Off-Axis'' mode.
 +
The ''dV'' parameter should be about ''3.15k'' at this point.
 +
Select IMFD in the right MFD also.
 +
  Click '''MNU''', then '''PG'''. Enter '''0''' for the ''MFD ID''. Click '''Map'''.
 +
Click '''Tgt''', and enter '''Moon'''. Click '''PG''', then '''Plan'''.
 +
Clidk '''PG''', then click '''Sel''' until Ref Moon appears in yellow text.
 +
Click '''MOD''' 3 times, then click '''Nxt''' so that ''Accuracy'' is highlighted.
 +
Click '''-''' twice so that ''accuracy'' is set to ''Max''.
 +
Click '''MOD''' twice to return to the map display with equatorial parameters.
 +
Wait until the ''TEj'' parameter in the left display is ''1k'' or less.
 +
In the left MFD, Click '''MOD''', and ''Offset Disabled'' should be highlighted.
 +
Click '''+''' twice and ''Vel. Frame'' should be displayed. Click '''Nxt''' until ''Lon'' is highlighted.
 +
Click '''Set''' and enter '''65'''. Click '''Nxt''' and ''Lat'' should be highlighted.
 +
Click '''Set''' and enter '''-59.8'''. Click '''Nxt''', then '''Set''', and enter '''20.3M''' for ''Rad''.
 +
Adjust the ''Rad'' and ''Lat'' parameters to get the ''PeA'' and ''EqI'' parameters in the right MFD as close
 +
as possible to ''350k'' and ''90'' degrees. Repeat as necessary. Click '''Pg''', then '''BV''', then '''AB'''.
 +
Disengage the ''Prograde'' autopilot.
 +
 
 +
[[Image:Lrotli.jpg|frame|left|IMFD setup for the TLI burn]] [[Image:Lrotli2.jpg|frame|right|IMFD setup for the TLI burn]]
 +
 
 +
 
  
Sit back and wait for the burn. You may wish to use time acceleration to get close to the burn time, but set it back to 1x acceleration once you get close.
 
  
''Note for Brian: It may be possible to use an offset in IMFD to target a polar orbit in the TLI. I think AMSO does something like this. It might be worth checking out, but it may make the LCROSS targeting harder. ''
 
  
When the TLI burn is complete, click on the '''BV''' button to restore the main IMFD Course target intercept screen
 
  
'''Do not jettison LRO yet'''
 
  
=== Lunar targeting/LRO ===
 
  
When you reach 32M altitude above the Earth, a piece of orbital debris will puncture the fuel tank of the centaur and drain all of its fuel. It is '''critical''' that you get your targeting done for both LRO and LCROSS before this time, as once that happens, your deltaV budget is severely limited.
 
  
At about 21M altitude above the earth, select TransX in the Right MFD.
 
  
Click on the '''--''' button until the target is ''Moon''
 
Click '''VW''' once so the View is ''Manoevre''
 
  
Select TransX also in the Left MFD.
 
  
In the Left MFD click '''FWD''', then '''VW''', so that the view is 'Encounter'
 
In the Right MFD click '''++''' so Manoevre mode is ''On''
 
Click '''VAR''' 5 times so that ''Ch. Plane vel.'' is displayed
 
Click '''ADJ''' so that ''Medium'' adjustment mode is entered.
 
Click '''--''' until the ''Min Alt.'' parameter in the Left MFD is over 50k
 
  
Our goal here is to end up with an ''Inclination'' parameter in the left MFD as close as possible to 90 degrees, and the ''Min Alt.''  parameter as close as possible to 50k.
 
  
In the Right MFD click '''VAR''' 3 times so that ''Prograde Vel'' is selected.
 
Click on '''ADJ''' 3 times  for ''Super'' adjustment mode.
 
Click on '''++''' or '''--''' until ''Min Alt.'' is close to 50k and ''Inclination'' is close to 90 degrees in the Left MFD.
 
  
Keep repeating these adjustments, using finer adjustment modes until you get as close as possible to the required parameters. Work quickly though, as the orbital debris is getting closer and we still have to target the LCROSS spacecraft.
 
  
In the Right MFD click '''VW''' to get ''Target view''
 
Use rotation mode to get the cross as close as possible to the center of the target.
 
'''Do NOT make the burn yet'''
 
  
Use the planetarium view '''F9''' key to make sure you are pointed in a generally northerly direction (towards Polaris + or - 30 degrees or so)
 
If you are pointed in a southerly direction, the transx targeting will have to be re-done using '''++''' Ch. plane vel. instead of '''--'''
 
  
Set the Left MFD to IMFD.
 
  
Press the '''MNU''' button and select Map mode.
 
Press the '''TGT''' button and enter '''Moon'''
 
Press the '''Sel''' button until ''Ref Moon'' is displayed.
 
  
Watch the PeA parameter as you make a low dV burn with the Centaur engine '''Ctrl-numpad +''' When the Pea gets to +50k, STOP the burn with the
 
'''numpad *''' key. As it gets close you may with to use translation mode and the '''numpad-6''' key. There is no reverse translation. Don't overshoot by very much, if at all. Some dV will be added by LRO jettison which we will have to correct later.
 
  
Press the '''j''' key to jettison LRO.
 
  
On the Right MFD click '''VW''' twice to get back to ''Maneuver view''
 
Click '''VAR''' until Maneuver Mode is displayed.
 
Click '''++''' to turn Maneuver mode ''Off''
 
  
=== Lunar targeting/LCROSS ===
 
  
* Swingby of moon is passive (no thrusting)
 
* 81 days in post-swingby cruise orbit
 
* Current baseline is 3-month trajectory with south pole impact
 
* Two revolutions in high ecliptic inclination (~50 deg), 40-day period Earth orbit
 
       
 
 
  
After the LRO is jettisoned, swing the Centaur around 180 degrees. Use the finely graduated scale on the hud, or Attitude MFD
 
to do this. When the Centaur is pointed 180 degrees from where it was when you made the LRO targeting burn, make another small burn, again watching
 
IMFD map so that the final PeA is about 2M on the opposite side of the moon. Select IMFD on the right MFD
 
  
Click '''MNU''', then '''Course'''. Click '''NXT''' 4 times so that ''Delta Velocity'' is highlighted. Click '''Set'''.
 
Click on '''TGT''' and enter '''Moon''' as the target. Click '''Nxt''' 5 times so that ''dVf'' is highlighted.
 
Click '''Set''' and enter '''0'''.
 
  
In the Left MFD click '''PG''' then '''Plan'''. The green line of our orbit should turn blue.
 
In the Right MFD click '''+''' repeatedly. The ''RIn'' parameter in the Left MFD should increase. If not, Click '''-''' until it does.
 
Also watch the ''PeA'' parameter. Do not let it go negative.
 
  
When ''PeA'' gets too low, click '''Nxt''' on the Right MFD so that ''dVp'' is highlighted.
 
Click '''-''' until ''PeA'' in the Left MFD is back to around 2M. Setting '''Adj''' to 10x may be necessary, but return it to 1x when finished.
 
  
Keep repeating these adjustments until ''Rin'' is close to 90 degrees and ''PeA'' is close to 2M. This is just a ball bark "rough in" to make our transx tageting easier. The numbers do not have to be exact. '''Work quickly''' though. Liberal use of the '''Pause''' function is encouraged.
 
  
  In the Right MFD, click '''Pg''', then '''BV'''.
+
Sit back and wait for the burn. You may wish to use time acceleration to get close to the burn time, but set it back to 1x acceleration once you get close.
 +
  When the TLI burn is complete, click on the '''BV''' button to restore
 +
the main IMFD Course target intercept screen. Click '''MOD''', then '''Prv'''
 +
until ''Vel. Frame'' is highlighted. Click '''+''' so that '''Offset Disabled''' is shown.
 +
Click '''MOD''' three times to return to the main target intercep screen.
 +
Also, in the right MFD, click '''Pg''', then '''Plan''' to disengage plan mode.
 +
 
 +
Press the '''j''' key to jettison LRO.
 +
Switch focus back to LRO.
 +
Press the '''k''' key to deploy the LRO solar panels
 +
Once the panels have fully unfolded, and rotated to face the sun,
 +
press the '''g''' key to deploy the antenna
  
Use rotation mode to align the cross in the center of the target and then select translation mode and use ''CTRL-numpad +''' to burn until ''BT'' is close to ''0''. AutoBurn is not recommended.
+
=== Lunar targeting/LCROSS ===
 +
* Swingby of moon is passive (no thrusting)
 +
* 84 days in post-swingby cruise orbit
 +
* Current baseline is a '''3 Lunar orbit:2 Spacecraft orbit''' trajectory with north pole impact
 +
* Two revolutions in high ecliptic inclination (~50 deg), 42-day period Earth orbit
  
Once this is done, in the Left MFD click '''PG''', then '''Plan''', so the orbit line turns green again.  
+
When you reach 32M altitude above the Earth, the Centaur engine will automatically purge of all fuel and control switches over to the LCROSS propulsion system. You may initate the engine purge manually by pressing '''B'''. It is '''critical''' that you get your targeting done for LCROSS before this time, as once that happens, your deltaV budget is severely limited.
  
Select Transx in both MFD's.Select moon as the target in the right MFD, as in the LRO targeting.
+
Switch focus to AV020Centaur. Select Orbit MFD in the right MFD.
 +
At about 21M altitude above the earth, select IMFD in the Right MFD.
 +
Click '''MNU''', then '''Map'''. Make sure Target is ''Moon'', and ''Ref moon'' is displayed.
 +
Click '''MOD''' three times, and set ''Accuracy'' to ''Max''.
 +
Click '''MOD''' again to return to the map display.
 +
Use rotational thrusters to point the Centaur in a northward direction. (Towards Polaris)
 +
Switch to translation mode and use linear thrusters until PeA in the Right MFD is about 2M.
 +
In the left MFD be sure ''Target Intercept'' is highlighted.
 +
Click '''+''', then '''Nxt''' four times until ''Delta Velocity'' is highlighted.
 +
Click '''Set'''. Click '''TGT''', and type '''Moon'''.
 +
Click '''Nxt''', then '''Set''', and set ''TEj'' to '''400'''.
 +
Click '''Nxt''' three times until ''dVf'' is highlighted.
 +
Click '''Set''', and enter '''0'''.
 +
in the Right MFD, click '''Plan''' so the green course line turns blue.
 +
In the left MFD, adjust ''dVp'' and ''dVf'' so that ''RIn'' and ''PeA'' in the right MFD
 +
are as close as possible to ''90'' degrees, and ''1.5M'', respectively.
 +
Click '''Prv''' until ''TEj'' is highlighted and set it to '''0'''.
 +
Click '''PG''', '''BV''', and '''AB'''.
 +
When the burn is finished, click '''BV''', and '''PG''' in the left MFD, and '''Plan''' in the right MFD.
 +
Select Transx in both MFDs.
 +
Select moon as the target in the right MFD
  
 
  Click the '''FWD''' button for stage 2, make sure the view is ''Setup'' and select the target as ''Escape''.
 
  Click the '''FWD''' button for stage 2, make sure the view is ''Setup'' and select the target as ''Escape''.
Line 174: Line 275:
  
 
There will be a green line extending from the center of the moon to hopefully past the edge. This is an edge-on view of our current approach to the moon.
 
There will be a green line extending from the center of the moon to hopefully past the edge. This is an edge-on view of our current approach to the moon.
We need to fine tune this approach to give us a lunar gravity assist which will result in a highly inclined orbit around the earth with a period of 40 days
+
We need to fine tune this approach to give us a lunar gravity assist which will result in a highly inclined orbit around the earth with a period of 42 days
  
 
  On the Right MFD, click the '''VAR''' button twice to bring up the ''Inc. angle'' parameter
 
  On the Right MFD, click the '''VAR''' button twice to bring up the ''Inc. angle'' parameter
  Click on '''--''' several times until the dotted yellow orbit is about the same size as the solid green line.  
+
  Click on '''++''' several times until the dotted yellow orbit is about the same size as the solid green line.  
 
  It does not have to be superimposed in the same place, but of a similar diameter.
 
  It does not have to be superimposed in the same place, but of a similar diameter.
  
 
On the Left MFD the dotted yellow line should be on the same side (more or less) of the moon as the green line. If it is on the opposite side,
 
On the Left MFD the dotted yellow line should be on the same side (more or less) of the moon as the green line. If it is on the opposite side,
click on the '''++''' button until it is on the same side.
+
click on the '''--''' button until it is on the same side.
  
 
  On the Right MFD, click on '''VAR''' four times until the ''outward angle'' parameter is shown.
 
  On the Right MFD, click on '''VAR''' four times until the ''outward angle'' parameter is shown.
  Adjust this parameter, and the Inc. angle parameter until the dotted line is superimposed on the solid green line in the slingshot view.
+
  Adjust this parameter, and the Inc. angle parameter until the dotted line is superimposed  
 
+
on the solid green line in the slingshot view.
This is our current trajectory. Now we need to adjust the trajectory to impact the moon in 2 orbits with a 40 day period.
 
  
 +
This is our current trajectory. Now we need to adjust the trajectory to impact the moon in 2 orbits with a 42 day period.
 +
Note the angle of this line. We will be adjusting the length of the line,
 +
but the angle '''must''' remain the same so that our flight path
 +
is over the moons pole.
 
  On the Right MFD, click '''VW''' so that the setup view is shown
 
  On the Right MFD, click '''VW''' so that the setup view is shown
 
  Click '''VAR''' 3 times so that ''Orbits to Icept'' is shown
 
  Click '''VAR''' 3 times so that ''Orbits to Icept'' is shown
 
  Click '''++''' 4 times so that the ''Orbits to Icept'' parameter is 2.0
 
  Click '''++''' 4 times so that the ''Orbits to Icept'' parameter is 2.0
  
Now we must figure out what our ''Enc. MJD'' should be. Take the current MJD and add 85 to it. (5 days to reach the moon, then 2 orbits of 40 days each.) For the Feb 28 (UTC) launch this would be 54890 + 85 = 54975. This is the ''Enc. MJD'' we will be shooting for.
+
Now we must figure out what our ''Enc. MJD'' should be. Take the current MJD and add 88.5 to it. (4.5 days to reach the moon, then 2 orbits of 42 days each.) For the 27 April(UTC) launch this would be 54948.2 + 88.5 = 55036.7 . This is the ''Enc. MJD'' we will be shooting for.
  
 
  Click '''VW''' again in the right MFD to get back to ''sling direct'' view.
 
  Click '''VW''' again in the right MFD to get back to ''sling direct'' view.
 
  Adjust the Inc Angle to get as close as possible to the desired MJD.
 
  Adjust the Inc Angle to get as close as possible to the desired MJD.
  Click '''VAR''' so that ''Outward angle'' is displayed.  
+
  When the angle strays too much,
  Click '''ADJ''' twice so that the increment is ''Fine''  
+
click '''VAR''' so that ''Outward angle'' is displayed.
 +
Adjust ''Outward angle'' to bring the lines back into alignment.
 +
Repeat the above process, until the date is as close as possible
 +
to the target date.  
 +
  Click '''ADJ''' so that the increment is ''Fine''  
 
  Adjust ''Outward angle'' to get the Cl. App. as close as possible.  
 
  Adjust ''Outward angle'' to get the Cl. App. as close as possible.  
  
My current solution is Inc Angle of -115.18 degrees and Outward angle of -47.54. Enc MJD is 54978.5013, and Cl. App is 1.747M<br>
+
My current solution is Inc Angle of 110.99 degrees and Outward angle of -38.1864. Enc MJD is 55036.6951, and Cl. App is 6.726M<br>
 
Your Mileage may vary.
 
Your Mileage may vary.
  
Once a solution has been reached, click '''BCK''' twice on the Right MFD. The View should be ''Maneuver'' and Maneuver mode should
+
[[Image:Lcrtgt2.jpg|frame|left|Transx Stage 2]][[Image:Lcrtgt3.jpg|frame|right|Transx stage 3]]
be ''off''. Click '''++''' to turn Maneuver mode ''on''
+
 
Adjust Prograde Vel. and Ch. Plane vel. until the dotted yellow line on the Left MFD lines up with the solid green line.
+
 
R. Inc should be as close as possible to 0, and Pe Ratio should be as close as possible to 1.000.
+
 
Once this is done, click '''VW''' in the right MFD to get to ''target view''.
+
 
Use rotational thrusters to get the cross in the middle of the target and burn until ''Rel.V'' is as close to 0 as possible.
+
 
Click '''VW''' twice to get to maneuver view, Click '''VAR''' to get to ''Maneuver mode'' and turn it off.
+
 
Look at the Left MFD to see how you did. Additional corrections may be done as you get closer to the moon.
+
 
 +
 
 +
 
 +
 
 +
 
  
=== Mid course correction/LRO ===
 
  
Switch focus back to LRO.
 
  
Press the '''k''' key to deploy the LRO solar panels
 
Once the panels have fully unfolded, and rotated to face the sun,
 
press the '''g''' key to deploy the antenna
 
  
In the Left MFD select IMFD, click on MNU and select Map.
 
Make sure TgT is Moon, and click Sel until Ref is Moon.
 
  
Wait until PeT is about 350k<br>
 
Select IMFD in the Right MFD
 
  
Click on '''MNU''', then '''Course'''. Click '''Nxt''' 4 times until ''Delta Velocity'' is highlighted, then click '''Set'''.
 
Click '''Nxt''' 5 times until ''dVf'' is highlighted, click '''Set''' and enter '''0'''.
 
Click on '''TgT''' and enter '''Moon'''.
 
In the Left MFD, click '''Pg''', then '''Plan''' so that the green line turns blue.
 
In the right MFD adjust '''dVp''' and '''dVf''' so that ''RIn'' and ''PeA'' in the left MFD are as close as possible to 90 degrees and 50k respectively
 
When these adjustments are finished, click '''PG''','''BV''', then '''AB''' in the right MFD.
 
When the burn completes, click '''Plan''' in the left MFD so the blue line returns to green.
 
  
Repeat these adjustments as necessary as you get closer to the moon.
 
  
=== Course correction/LCROSS ===
 
Switch focus to AV020 Centaur. Select TranxX in both left and right MFDs
 
  
In the right MFD, click '''++''' to turn Maneuvre mode ''On''.
 
Adjust ''Prograde vel'' and ''Ch. plane vel'' so that on the Left MFD ''R. Inc'' is as close as possible to 0,
 
and ''Pe Ratio'' is as close as possible to 1.0
 
Click '''VW''' on the right MFD for ''Target view''. Use rotational thrusters to get the cross as close to the
 
center of the target as possible. Press '''M''' to enable the dummy main engine, and use the '''numpad-+''' key to
 
burn the engine. Reduce the ''Rel V'' to as close to 0 as possible.
 
  
As an alternative to using the dummy main engine, after the Centaur is targeted with rotational thrusters, you can
 
rotate the Centaur 180 degrees and use the LCROSS main engine '''numpad--''' (minus) This will provide you with graphics
 
of the engine firing in external view. ('''F1''')
 
  
Repeat these adjustments as necessary as you get closer to the moon.
 
  
=== orbit insertion/LRO ===
 
  
The LRO main engine is not strong enough to get it into a circular orbit in one try. It will take 3 orbits to achieve a 50km circular orbit. The first burn is critical in that we must avoid a situation where we are "weakly captured" or not captured at all. The orbit eccentricity at the end of our first burn must be 0.8 or less.
 
  
When LRO's PeT is about 10k, select imfd in the left MFD, and orbit MFD in the right.
 
Click on the '''HUD''' button on the right MFD. In the left MFD click '''MNU''', then '''Orbital'''.
 
Click '''TgT''', then type '''r'''.
 
Note that The burn time to a circular orbit is over 4k seconds (over an hour!). Make sure rotational mode is selected.
 
At 2k seconds to PeT, select Retrograde mode on the hud. When retrograde attitude is established, de-select retrograde mode.
 
Start the engine by pressing '''numpad-+''' and tap the '''CTRL''' key to keep it burning.
 
Notice that the PeA in the right MFD is decreasing.
 
Use the numpad '''1''' and '''3''' keys to move the attitude closer to what the Orbital imfd mode thinks it should be until
 
the PeA starts increasing.
 
Keep adjusting the attitude between these points to keep the PeA as close as possible to 50k.
 
When the Ecc. parameter in the Right MFD is less than 0.8, press the '''numpad-*''' key to stop the burn.
 
Switch focus to AV020Centaur and enjoy the view as it passes by the moon. After the flyby, switch back to LRO and wait until PeT
 
is 1.5k. Press the retrograde button, and de-select it when retrograde attitude is achieved.
 
Follow the procedure above to make the second burn, keeping PeA as close as possible to 50k, and burn until Eccentricity is below 0.4
 
Stop the burn when Eccentricity is below 0.4
 
Go another orbit around the moon, and wait until PeT is 600 seconds.
 
Assume retrograde attitude again, and then de-select the retrograde autopilot. Burn again, keeping PeA as close as possible to 50k
 
until Eccentricity is as close as possible to 0. Stop the burn immediately when a circular orbit is reached.
 
  
=== LCROSS orbit correction 1 ===
 
Switch focus back to AV020Centaur and wait until the orbit is farthest from the moon. '''WARNING''' Using High values of time acceleration may cause problems for the LRO orbit. It can even kick it out of lunar orbit. It is best to be patient, and check on LRO's orbit once in a while. If it's orbit
 
changes significantly due to time acceleration, fix it with scenario editor. It is now necessary to tune IMFD map for maximum accuracy.
 
Select IMFD in the left MFD. Click '''MNU''', then '''Map'''. Click '''TgT''' and type '''Moon''', Click '''Cnt''', and type '''Earth'''.
 
Click '''MOD''' 3 times. This should give you the Map-config screen. ''Legs/Frame'' should be highlighted. Click '''Set''' and type '''64'''.
 
Click '''Nxt''', then '''-''' twice. Click '''Nxt twice again, so that ''Period limit'' is highlighted, and click '''+''' to turn it off.
 
Click '''Nxt''' and '''+''' to turn ''Hyper limit'' off. Click '''Nxt''' twice and then '''+''' so that ''Tgt weak Pe'' is set to No.
 
Click '''Nxt''' and '''+''' to turn ''One Pe/Ref'' off. Click '''Mod''' again to return to the map display.
 
Several orbits should now be shown. Select IMFD in the Right MFD.
 
In the right MFD click '''MNU''', then '''Course'''. Select ''Delta Velocity'' mode, then set the target to Moon. Set the ''dVf'' parameter to 0.
 
In the left MFD click '''PG''', then '''Plan'''. in the right MFD, adjust '''dVf''' to get the most deflection of the orbit you can when
 
LCROSS intersects the moon in 1.5 orbits. When this is done, click on '''Pg''', then '''BV''', then '''AB'''.
 
When the burn is finished, click '''Plan''' in the left MFD to turn the orbit line green again.
 
  
=== LCROSS final moon targeting ===
 
=== LCROSS pole targetinjg ===
 
=== LCROSS LRO targeting ===
 
* ~7 hours prior to impact, LCROSS will separate from Centaur upper stage and perform a ~10-minute delay maneuver (~30 m/s)  to enable LCROSS to fly through Centaur impact plume
 
  
== External reference documents ==
+
Once a solution has been reached, click '''BCK''' twice on the Right MFD.
 +
The View should be ''Maneuver'' and Maneuver mode should
 +
be ''off''. Click '''++''' to turn Maneuver mode ''on''
 +
Adjust Prograde Vel. and Ch. Plane vel. until the dotted yellow line on the Left MFD
 +
lines up with the solid green line.
 +
R. Inc should be as close as possible to 0, and Pe Ratio should be as close as possible to 1.000.
 +
Once this is done, click '''VW''' in the right MFD to get to ''target view''.
 +
Use rotational thrusters to get the cross in the middle of the target and burn until
 +
''Rel.V'' is as close to 0 as possible.
 +
Click '''VW''' twice to get to maneuver view, Click '''VAR''' to get to ''Maneuver mode'' and turn it off.
 +
Look at the Left MFD to see how you did. Additional corrections may be done as you get
 +
closer to the moon.
  
[http://lcross.arc.nasa.gov/docs/astrWorkshop/Galal_Orbit_Design_Galal_Final.ppt LCROSS Astronomer Workshop]<br>
+
== See also ==
[http://lcross.arc.nasa.gov/ NASA LCROSS page]<br>
+
*[[Lunar Reconnaissance Orbiter]]
[http://lunar.gsfc.nasa.gov/ NASA LRO page]<br>
+
*[[Lunar Reconnaissance Orbiter part 2]]
[http://lroc.sese.asu.edu/ ASU LRO Camera Page]<br>
 
[http://trs-new.jpl.nasa.gov/dspace/bitstream/2014/40781/1/06-2277_A.pdf Trajectory Design of the Lunar Impactor Mission Concept]<br>
 
[http://lunar.gsfc.nasa.gov/library/tooley-scobjectives-51906.pdf Lunar Reconnaissance Orbiter Spacecraft & Objectives]<br>
 
[http://lunar.gsfc.nasa.gov/library/IAC-07-C1_7_06.pdf Mission Design And Operations Considerations For NASA’S LRO]<br>
 
  
== TODO ==
+
[[Category:Articles]]
*Fix procedure for actual mission parameters
+
[[Category:Orbiter 2010 add-ons]]
** updated Launch date
+
[[Category:Spacecraft add-ons]]
** LCROSS North pole impact
+
[[Category:Add-ons by BrianJ]]
** Try IMFD slingshot mode to refine flyby once in lunar SOI
+
[[Category:Tutorials]]
** LRO lunar insertion orbits
 
* Add keyboard commands section
 
* Convert to .CHM for help mode within orbiter
 
* Add images
 
** IMFD map periapsis projection to show LCROSS orbit inclination
 

Latest revision as of 13:03, 8 November 2022

Overview[edit]

The Lunar Reconnaissance Orbiter (LRO) is the first mission in NASA's planned return to the moon. LRO is scheduled to launch 24th April, 2009, with the objectives to finding safe landing sites, locate potential resources, characterize the radiation environment and test new technology.

The return to the moon will enable the pursuit of scientific activities that address our fundamental questions about the history of Earth, the solar system and the universe -- and about our place in them. It will allow us to test technologies, systems, flight operation and exploration techniques to reduce the risk and increase the productivity of future missions to Mars and beyond. It will also expand Earth's economic sphere to conduct lunar activities with benefits to life on our home planet.

LRO is an unmanned mission to create the comprehensive atlas of the moon's features and resources necessary to design and build a lunar outpost. LRO focuses on the selection of safe landing sites, identification of lunar resources and the study of how lunar radiation will affect humans.

After launch, the LCROSS shepherding spacecraft and the Atlas V’s Centaur upper stage rocket will execute a fly-by of the moon and enter into an elongated Earth orbit to position LCROSS for impact on a lunar pole. On final approach, the shepherding spacecraft and Centaur will separate. The Centaur will act as a heavy impactor to create a debris plume that will rise above the lunar surface. Following four minutes behind, the shepherding spacecraft will fly through the debris plume, collecting and relaying data back to Earth before impacting the lunar surface and creating a second debris plume.

The debris plumes are expected to be visible from Earth- and space-based telescopes 10-to-12 inches and larger.

This is a difficult and challenging mission. Experienced orbinauts will enjoy the challenge of targeting the LCROSS to impact the North Pole of the moon, when the LRO spacecraft is overhead. This mission is not recommended for people recently starting to use Orbiter. Familiarity with setting up gravity assist maneuvers in TransX is a required skill.

Mission Objectives[edit]

LRO[edit]

The objective of the LRO mission is to map the lunar surface in preparation for the return of human missions to the moon, which are planned to occur by 2020.

LCROSS[edit]

Earth’s closest neighbor is holding a secret. In 1999, hints of that secret were revealed in the form of concentrated hydrogen signatures detected in permanently shadowed craters at the lunar poles by NASA’s Lunar Prospector. These readings may be an indication of lunar water and could have far-reaching implications as humans expand exploration past low-Earth orbit. The Lunar CRater Observing and Sensing Satellite (LCROSS) mission is seeking a definitive answer.

Required add-ons[edit]

Optional add-ons[edit]

Spacecraft Specifications[edit]

LRO

  • Empty Mass 809kg
  • Fuel Mass 897kg, ISP 2100Ns/kg
  • Main Engine 352N
  • RCS 20N


LCROSS

  • Empty Mass 592kg
  • Fuel Mass 300kg, ISP 2200Ns/kg
  • Retro Engine 44N
  • RCS 4.5N


AV020Centaur

  • Empty Mass 1914kg
  • Fuel Mass 20672kg, ISP 4200Ns/kg
  • Main Engine 99400N
  • RCS 1000N

NOTE: When AV020Centaur fuel is finished, control is automatically switched to LCROSS propulsion system.

Spacecraft Controls[edit]

Available commands are displayed on the top-left of the vessel HUD

AV020Centaur

P = Toggle Parking Orbit Autopilot On/Off
J = Jettison LRO
B = Manual Purge Centaur Fuel (automatic at 32000km alt.)
K = Jettison LCROSS
V = Deploy/Delete LCROSS "Bullseye" target on Moon N.Pole
N = Display LRO Lunar Orbit Data
M = TransX cheat! Enable 44N "ghost" Main Engine for use with TransX


LRO

G = Deploy Antenna (automatic Earth tracking)
K = Deploy Solar Panel (automatic Sun tracking)
N = Activate Laser Altimeter
V / ShiftV = Rotate DLRE Azimuth
B / ShiftB = Rotate DLRE Elevation


LCROSS

F8 = View from Visual Context Imager (6 deg FOV)


LC-41 (Launch Pad)

V = LOX Vent On/Off
K = Lights Off
NOTE: LC-41 is automatically deleted when focus vessel is above 100km alt.

Add-on Notes and Quick Info[edit]

NOTES

Moon Orientation
The precession of the Moon's axis is not modelled in Orbiter. To ensure accuracy of the Moon's orientation at the time of the mission, the LRO add-on uses a custom sol.cfg and moon.cfg located in the Config/LRO/ directory. To use them, the "Environment" entry in the scenario file must point to the LRO/sol.cfg. e.g.

BEGIN_ENVIRONMENT
 System LRO/Sol
 Date MJD 54892.2256944444
END_ENVIRONMENT


Launch Date
Although the launch is currently scheduled for 24th April 2009, the primary launch scenario provided in this add-on is the 27th April 2009 due to the mission constraints on the LAN of LRO's final Lunar orbit. The second launch scenario provided is for the 24th April 2009, should you wish to use it.

Transx version
This document assumes the default Transx version supplied with Orbiter. Other versions may give different lunar intercept times.


QUICK INFO

LRO
Final Lunar orbit - 30km x 70km, 90deg inclination(Equatorial), Periselene over South Pole,
LAN = 38deg(Ecliptic) +/- 17deg(max.)


LCROSS/AV020Centaur
Uses Lunar flyby to reach high-inclination Earth orbit,
Spacecraft:Moon orbit resonance 2:3 (other resonances possible)

Impact chosen target at North Pole of Moon (targets designated by surface bases "Lcross_A" to "Lcross_E"), impact speed ~2.5km/s, impact angle > 60deg.

Lcross separates from AV020Centaur at impact -9hrs. Lcross impact 4mins after AV020Centaur.

Impact should be timed to be visible by LRO passing over and by ground-based observers in Hawaii during hours of darkness.

Procedures[edit]

Accuracy of burns in this mission is CRITICAL.

Launch[edit]

Fire up the 01 - AV020 LRO launch 27Apr scenario in the LRO scenarios folder This is a night launch so visibility is poor until after the TLI burn. The scenario starts at UTC 04/27/2009 04:09:00. Launch time is UTC 04:10:11. The default camera view is Ground Observer. You have just over a minute to set up the camera to your personal preference.

At UTC 04:10:01 press the p key to start the launch countdown and 
1st stage auto-pilot.

At T-5 seconds, engine ignition will happen, and the hold down clamps release at T-0. The Atlas V-401 1st stage autopilot will continue until 1st stage seperation.It can be disengaged by Pressing p again, but this is not recommended.

10 seconds after 1st stage separation, press the p key again.

This will ignite the 2nd stage Centaur engine, and engage the 2nd stage autopilot which will put the vehicle in a circular 185km parking orbit. Pressing p again will disengage the 2nd stage autopilot.

Shortly after 2nd stage ignition, the fairing will be automatically jettisoned, and the LRO/LCROSS spacecraft will be exposed.

TLI[edit]

After SECO, while established in the 185km parking orbit, set the Left MFD to IMFD.

Also, click the HUD button in the right orbit MFD so that your HUD is set to orbit reference Earth
Click the Prograde button to engage the prograde autopilot. 

IMFD Configuration set-up[edit]

Click MNU, then Configuration. 
Click Nxt, then + to change the Mission timer to MJD mode. 
Click Nxt ten times to hightlight Parking Orbit Alt. 
Click Set, and set this to 185k

Establishing the TLI burn[edit]

Click MNU, then Course.
Target Intercept should be highlighted. If not, click Nxt until it is.
Click Set
Click Tgt and enter Moon
Click Nxt 6 times so that Off Plane is highlighted. 
Click + twice to change it to Source Plane.
Click Prv so that Realtime is higlighted. 
Click + to change it to Off-Axis
Click Prv twice so that TIn is highlighted.
Click + or - repeatedly to minimize the value of PlC in the lower left section of the MFD.
You may want to click on ADJ and set it to 10x for this adjustment.
Be sure to set it back to 1x when finished. 
Click Prv twice so the Tej parameter is highlighted.
Click + or - repeatedly until the EjA parameter is about 3 degrees. 
If you go much below 3 degrees the Off-Axis parameter will change back to Realtime,
and we need to be in Off-Axis mode. 
The dV parameter should be about 3.15k at this point.

Select IMFD in the right MFD also.

Click MNU, then PG. Enter 0 for the MFD ID. Click Map.
Click Tgt, and enter Moon. Click PG, then Plan.
Clidk PG, then click Sel until Ref Moon appears in yellow text.
Click MOD 3 times, then click Nxt so that Accuracy is highlighted. 
Click - twice so that accuracy is set to Max.
Click MOD twice to return to the map display with equatorial parameters.

Wait until the TEj parameter in the left display is 1k or less.

In the left MFD, Click MOD, and Offset Disabled should be highlighted. 
Click + twice and Vel. Frame should be displayed. Click Nxt until Lon is highlighted. 
Click Set and enter 65. Click Nxt and Lat should be highlighted. 
Click Set and enter -59.8. Click Nxt, then Set, and enter 20.3M for Rad. 
Adjust the Rad and Lat parameters to get the PeA and EqI parameters in the right MFD as close
as possible to 350k and 90 degrees. Repeat as necessary. Click Pg, then BV, then AB.
Disengage the Prograde autopilot.
IMFD setup for the TLI burn
IMFD setup for the TLI burn
















Sit back and wait for the burn. You may wish to use time acceleration to get close to the burn time, but set it back to 1x acceleration once you get close.

When the TLI burn is complete, click on the BV button to restore 
the main IMFD Course target intercept screen. Click MOD, then Prv
until Vel. Frame is highlighted. Click + so that Offset Disabled is shown.
Click MOD three times to return to the main target intercep screen.
Also, in the right MFD, click Pg, then Plan to disengage plan mode.
Press the j key to jettison LRO.
Switch focus back to LRO.
Press the k key to deploy the LRO solar panels
Once the panels have fully unfolded, and rotated to face the sun,
press the g key to deploy the antenna

Lunar targeting/LCROSS[edit]

  • Swingby of moon is passive (no thrusting)
  • 84 days in post-swingby cruise orbit
  • Current baseline is a 3 Lunar orbit:2 Spacecraft orbit trajectory with north pole impact
  • Two revolutions in high ecliptic inclination (~50 deg), 42-day period Earth orbit

When you reach 32M altitude above the Earth, the Centaur engine will automatically purge of all fuel and control switches over to the LCROSS propulsion system. You may initate the engine purge manually by pressing B. It is critical that you get your targeting done for LCROSS before this time, as once that happens, your deltaV budget is severely limited.

Switch focus to AV020Centaur. Select Orbit MFD in the right MFD. At about 21M altitude above the earth, select IMFD in the Right MFD.

Click MNU, then Map. Make sure Target is Moon, and Ref moon is displayed.
Click MOD three times, and set Accuracy to Max.
Click MOD again to return to the map display.
Use rotational thrusters to point the Centaur in a northward direction. (Towards Polaris)
Switch to translation mode and use linear thrusters until PeA in the Right MFD is about 2M.
In the left MFD be sure Target Intercept is highlighted. 
Click +, then Nxt four times until Delta Velocity is highlighted. 
Click Set. Click TGT, and type Moon.
Click Nxt, then Set, and set TEj to 400.
Click Nxt three times until dVf is highlighted. 
Click Set, and enter 0.
in the Right MFD, click Plan so the green course line turns blue.
In the left MFD, adjust dVp and dVf so that RIn and PeA in the right MFD
are as close as possible to 90 degrees, and 1.5M, respectively.
Click Prv until TEj is highlighted and set it to 0.
Click PG, BV, and AB.
When the burn is finished, click BV, and PG in the left MFD, and Plan in the right MFD.

Select Transx in both MFDs. Select moon as the target in the right MFD

Click the FWD button for stage 2, make sure the view is Setup and select the target as Escape.
Click the FWD button again for stage 3, and select the target as Moon
Click the VW button for Sling Direct view.
On the Left MFD, click the FWD button for stage 2, if not already there. 
Click the VW button for slingshot view, if not already there.

There will be a green line extending from the center of the moon to hopefully past the edge. This is an edge-on view of our current approach to the moon. We need to fine tune this approach to give us a lunar gravity assist which will result in a highly inclined orbit around the earth with a period of 42 days

On the Right MFD, click the VAR button twice to bring up the Inc. angle parameter
Click on ++ several times until the dotted yellow orbit is about the same size as the solid green line. 
It does not have to be superimposed in the same place, but of a similar diameter.

On the Left MFD the dotted yellow line should be on the same side (more or less) of the moon as the green line. If it is on the opposite side, click on the -- button until it is on the same side.

On the Right MFD, click on VAR four times until the outward angle parameter is shown.
Adjust this parameter, and the Inc. angle parameter until the dotted line is superimposed 
on the solid green line in the slingshot view.

This is our current trajectory. Now we need to adjust the trajectory to impact the moon in 2 orbits with a 42 day period.

Note the angle of this line. We will be adjusting the length of the line,
but the angle must remain the same so that our flight path
is over the moons pole.
On the Right MFD, click VW so that the setup view is shown
Click VAR 3 times so that Orbits to Icept is shown
Click ++ 4 times so that the Orbits to Icept parameter is 2.0

Now we must figure out what our Enc. MJD should be. Take the current MJD and add 88.5 to it. (4.5 days to reach the moon, then 2 orbits of 42 days each.) For the 27 April(UTC) launch this would be 54948.2 + 88.5 = 55036.7 . This is the Enc. MJD we will be shooting for.

Click VW again in the right MFD to get back to sling direct view.
Adjust the Inc Angle to get as close as possible to the desired MJD.
When the angle strays too much, 
click VAR so that Outward angle is displayed. 
Adjust Outward angle to bring the lines back into alignment. 
Repeat the above process, until the date is as close as possible
to the target date. 
Click ADJ so that the increment is Fine 
Adjust Outward angle to get the Cl. App. as close as possible. 

My current solution is Inc Angle of 110.99 degrees and Outward angle of -38.1864. Enc MJD is 55036.6951, and Cl. App is 6.726M
Your Mileage may vary.

Transx Stage 2
Transx stage 3















Once a solution has been reached, click BCK twice on the Right MFD. 
The View should be Maneuver and Maneuver mode should
be off. Click ++ to turn Maneuver mode on
Adjust Prograde Vel. and Ch. Plane vel. until the dotted yellow line on the Left MFD 
lines up with the solid green line. 
R. Inc should be as close as possible to 0, and Pe Ratio should be as close as possible to 1.000.
Once this is done, click VW in the right MFD to get to target view.
Use rotational thrusters to get the cross in the middle of the target and burn until 
Rel.V is as close to 0 as possible.
Click VW twice to get to maneuver view, Click VAR to get to Maneuver mode and turn it off.
Look at the Left MFD to see how you did. Additional corrections may be done as you get 
closer to the moon.

See also[edit]